Buy XW20058M1 Part of Rosemount Aerospace Inc with NSN 6105-00-630-5828
MPN: XW20058M1
Manufacturer: Rosemount Aerospace Inc
NSN: 6105-00-630-5828
Item Name: Motor Direct Curren
CAGE Code: 59885
Part number XW20058M1 is available for immediate shipping. The NSN for part number is 6105006305828. This part is manufactured by Rosemount Aerospace Inc. It is described as Motor Direct Curren. Would you like to request a quote for part number XW20058M1? Please fill out the form.
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NSN Information for Part Number XW20058M1 with NSN 6105-00-630-5828, 6105006305828
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
6105-00-630-5828 Item Description: Motor Direct Curren | 6105 | 006305828 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Xw20058m1 | 2 | 2 | 5 |
Characteristics Data of NSN 6105-00-630-5828, 6105006305828
MRC | Criteria | Characteristic |
---|---|---|
AAJT | OVERALL HEIGHT | 3.540 INCHES |
AAJU | III OVERALL LENGTH | 5.500 INCHES |
AAJV | OVERALL WIDTH | 3.890 INCHES |
AKCT | SHAFT ROTATION DIRECTION | CLOCKWISE SINGLE END |
AKPS | DUTY CYCLE | CONTINUOUS |
ANPZ | INCLOSURE FEATURE | TOTALLY INCLOSED |
AXCP | WINDING TYPE | SERIES WOUND |
AXGY | MOUNTING METHOD | FIXED BASE |
BFMF | COOLING METHOD | AMBIENT AIR |
CNXS | POWER RATING | 0.1250 HORSEPOWER OUTPUT |
CRTL | CRITICALITY CODE JUSTIFICATION | SUPP |
CWCS | LENGTH OF SHAFT FROM HOUSING | 0.062 INCHES SINGLE END |
CWFX | ROTOR SPEED RATING IN RPM | 11600.0 SINGLE NO LOAD |
CWGL | CURRENT RATING IN AMPS | 5.200 SINGLE INPUT |
CWGQ | CONNECTION TYPE AND VOLTAGE RATING IN VOLTS | 27.0 LINE TO NEUTRAL SINGLE INPUT |
FEAT | SPECIAL FEATURES | MOUNTING FACILTIY: THROUGH-HOLE, 2 X 0.265; ROTOR SPEED RATING: HIGH SPEED = 11,800 RPM; SHAFT CHARACTERISTICS: SQUARE (0.150 +.000/-003 X 0.13 LONG), SINGLE ENDED; TERMINAL TYPE AND QUANTITY: RECEPTACLE, MS3102A10SL-3P |
SUPP | SUPPLEMENTARY FEATURES | AVIATION CRITICAL SAFTY/FLIGHT SAFTY CRITICAL AIRCRAFT PART |
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